Turbine generator

Abstract: The rotor 2 of a rotating field type turbine generator is provided with slots 3 for accommodating the field windings, wedges 4 positioned at the portions of the magnetic poles on the rotor 2 for holding the field windings and wedges 5 positioned between the magnetic poles on the rotor. These wedges 4 and 5 are constituted by metal bars without joints to enhance damper effect thereby. Magnetomotive forces due to higher harmonics, which causes temperature rise of the rotor 2 and torque ripple during starting with thyristors, induces an elliptic rotating magnetic field having the longer diameter on d axis extending in the direction of magnetomotive force induced by the field windings and the shorter diameter on q axis perpendicular to d axis, and thus a larger eddy current is induced flowing along q axis on the rotor 2 than that flowing along d axis. Therefore the thickness d' in radial direction of the wedges 5 positioned between the magnetic poles on the rotor 2 is determined larger than the thickness d in radial direction of the wedges 4 positioned at the portions of the magnetic poles on the rotor 2 to reduce the resistance of the wedges 5 and to easily lead the eddy current flowing in the axial direction of the rotor 2, thereby a good thermal balance over the entire portions on the rotor 2 is achieved.

Description: The present invention relates to a turbine generator and, in particular, relates to a turbine generator which is suitable for starting a gas turbine, acting as a variable speed synchronous motor by connecting armature windings of the turbine generator with a thyristor type starting device. These days, combined cycle electric power generation has drawn attention in view of its energy efficiency. Fig. 2 shows a constitution diagram of a combined cycle electric power generation system. It consists of a gas turbine 10, a steam turbine 11 which uses heat in the exhaust from the gas turbine 10 as heat source for a turbine generator 12 and a boiler (not shown). A gas turbine 10, steam turbine 11 and turbine generator 12 are arranged along a common axis as a single element, and to provide greater capacity, a single plant is generally composed of an array of such elements. Such a combined cycle electric power generation plant is usually located near urban area heaving a large electric power demand and is operated on DSS ( D aily S tart and S top) basis, in that gas turbines 10 are successively started dependent upon the load demanded of the plant. The general trend toward increasing the gas turbine combustion temperature to achieve higher efficiency results in the capacity of the gas turbine in the combined cycle electric power generation plant increasing, and accordingly the capacity of the starting device for the gas turbine must be increased. In a conventional starting device for starting the gas turbine, a torque converter system is used in which a torque converter and an induction motor is directly coupled at a power train axial end. However, because of limits on the manufacturable size of the torque converter, increases in the capacity the starting device eventually become difficult. Attention is therefore directed to alternative, thyristor type, starting system. The thyristor type starting system is one in which the turbine generator 12 is started as a variable speed synchronous motor by making use of a thyristor type starting device 13. Through provision of a change-over device 1 between the turbine generators 12 and the thyristor starting device 13, a single thyristor starting device 13 can be used for all elements of the array. Therefore, a more compact building can accommodate all of the necessary devices. In a conventional generator, the rotor is provided with field windings which excite the generator while receiving a DC current from a suitable current source, and the stator thereof is provided with armature windings from which an electrical power is output. In such a generator, when an unbalanced load condition occurs, in which load conditions in respective phases of the three phase armature windings are different, a negative phase rotating magnetic field is generated in the rotor due to the unbalanced armature current. The negative phase rotating magnetic field contains an asynchronous magnetic field component composed of a single component having an angular frequency 2w, i.e. twice the angular frequency ω of the output voltage. When such a negative phase rotating magnetic field is generated, an eddy current is induced in respective conductor portions on the rotor and temperatures at the respective portions on the rotor rise beyond a predetermined allowable limit. Accordingly, to try and resolve the above problem, JP-B-60-34340(1985) proposes that current flowing in axial direction on the solid iron core rotor is led toward damper windings via conductive wedges and thereby a thermal balance at respective portions on the rotor is achieved. JP-A-60-229640 (1985) proposes another measure in which resistance values of damper bars inserted into slots on the rotor are varied and thereby a thermal balance at respective portions on the rotor is achieved. Specifically, this document proposes relatively thicker damper bars at the poles of the rotor, and thinner damper bars at intermediate locations. To explain the theory behind the present invention, reference will be made to Figs. 3 to 6. Fig. 3 shows a turbine generator system constitution diagram in which the turbine generator is started by a thyristor type starting device. Figs. 4(a) and 4(b) show the armature current fed from the thyristor type starting device, and Fig. 5 shows the relationship of magnetomotive force vectors induced in the machine during starting. Fig. 6 shows a magnetomotive force of a sixth order higher harmonic wave induced during starting by the thyristor type starting device. In these drawings, numeral 14 denotes an exciter, CONV a converter, INV an inverter, numeral 2 a rotor of the turbine generator 12, numeral 3 slots provided on the rotor 2 for accommodating field windings. In the thyristor type starting system, since the turbine generator 12 acts as a variable speed synchronous motor during starting, it is necessary to form a rotating magnetic field of variable frequency at the armature side. Accordingly, during starting with thyristors the thyristor type starting device 13 constituted by the inverter INV and the converter CONV is connected for feeding a balanced three phase AC current of variable frequency to the armature winding thereof, and the field windings thereof are excited by DC current. The variable frequency of the balanced three phase AC current from the thyristor type starting device 13 is adjusted to one which is synchronous with the rotating frequency of the rotor 2 and is designed to increase dependent upon increase of the rotating speed. The current fed to the armature windings from the thyristor type starting device 13 in such instance is in a distorted waveform as shown in Fig.4(a). As illustrated in the current waveforms, in order to maintain a condition wherein two phases among the three phases are always in a conductive state, the respective phases (U phase, V phase and W phase) each repeat in a corresponding manner, i.e. a positive polarity conductive state of 120° electrical angle, a rest state of 60° electrical angle, a negative polarity conductive state of 120° electrical angle and a rest state of 60° electrical angle. The spectrum of the current waveform of 120° electrical angle conduction is shown in Fig.4(b), wherein apart from the current component of the fundamental waveform, higher harmonic current components of (6m±1)th order are contained in the current fed to the armature windings of the turbine generator 12 from the thyristor type starting device 13. Further, during starting with thyristors the magnetomotive force Fa of the armature fundamental wave is designed to be perpendicular with respect to the magnetomotive force Ff of field windings in order to maximize torque to be generated as illustrated in Fig.5. In this instance, since higher harmonic components of (6m±1)th order are contained in the armature current as explained above, magnetomotive force of high harmonics of 6mth order are generated in the machine when looking from the rotor side, together with elliptic rotating magnetic fields with their longer diameter on the d axis and the shorter diameter on the q axis. The formation of the elliptic rotating magnetic fields can be explained with reference to Fig. 6 wherein an example when m=1, in that, the magnetomotive force of higher harmonic of 6th order is taken up. Although the higher harmonics components of 5th and 7th orders in the armature current form magnetomotive forces of 5th and 7th order higher harmonics when looking from the stator side, the magnetomotive force of 5th order higher harmonic rotates in opposite direction with respect to the rotating direction of the rotor 2 to thereby constitute a magnetomotive force of 6th order higher harmonic when looking at the rotor 2 and the magnetomotive force of 7th order higher harmonic rotates in the same direction with the rotating direction of the rotor 2 to thereby constitute magnetomotive force of 6th order higher harmonic when looking at from the rotor 2. As will be understood from the above, the magnetomotive force of 6th order higher harmonic is consisted of two vector components and the two vector components show the same direction on d axis, therefore the resultant vector on d axis is the sum of the two vector components, however since there two vector components rotate in opposite directions each other, these two vector components show opposite directions on q axis, therefore the resultant vector is the difference between the two vector components. Thus, the sum of these two vector components shows an elliptic form having the longer diameter on d axis and the shorter diameter on q axis as illustrated in Fig. 6. The ratio of d and q axis components of the 6th order higher harmonic is usually at 6m : 1. Now, when an asynchronous magnetic field is generated, an eddy current is induced over the surface of the rotor so as to suppress the asynchronous magnetic field. Generators now in use are provided with damper bars which are arranged uniformly over the rotor, without regard to the position of the magnetic poles, in order to optimumly suppress an asynchronous magnetic field consisting of a single component such as a negative phase rotating magnetic field which is generated during unbalanced loading. However, the inventors found out that in case of an asynchronous magnetic field consisting of a plurality of components such as experienced during starting with thyristors a larger eddy current is induced on the rotor portions between the magnetic poles in comparison with one on the rotor portion at the magnetic poles, in the resistance loss distribution over the rotor surface n circumferential direction becomes non-uniform and thus an optimum damper effect cannot be achieved. The present invention is made in view of the above problem, and thus seeks to provide a turbine generator which achieves thermal balance over the entire rotor surface of the generator during starting with thyristors and preferably reduces the required starting time significantly. Toward achieving this aim, it proposes constituting the rotor in such a manner that the resistance loss distribution over the entire rotor surface in circumferential direction is uniformalized by varying the physical properties around the circumference of the rotor. One method of achieving this is by providing wedges or damper bars, inserted into slots to contain field windings therein and give rise to damping effect, thereby to maintain a thermal balance over the entire rotor surface by varying the physical properties or configuration of the wedges or damper bars dependent on their circumferential position. Accordingly, the present invention provides a turbine generator as set forth in claim 1. The present invention lies in recognising the non-uniformity of the induced magnetic field arising from higher harmonics of the armature current, and varying the resistance offered to eddy currents so as to reduce excessive variation in resistive heating across the surface of the rotor. Defining the d and q axes as above, a suitable variation of the properties of the wedges or damper bars is chosen to reduce the resistance of the wedges or damper bars positioned proximate the q axis of the rotor relative to the resistance of the wedges or damper bars positioned proximate the d axis of the rotor. To do this the circumferential properties of the rotor can be varied by varying the physical properties or the configuration of damper bars which are provided together with the field windings so as to maintain a thermal balance over the entire rotor surface via the damper bars. The variation of physical properties or configuration is preferably one of the following: (i) providing that the radial thickness of the wedges or damper bars proximate the d axis is less than the radial thickness or th wedges proximate tne q axis, (ii) providing that the resistivity of the wedges or damper bars proximate the d axis is greater than the resistivity of the damper bars proximate the q axis, (iii) providing that the circumferential width of the wedges or damper bars proximate the d axis is less than the circumferential width of the wedges or damper bars proximate the q axis, (iv) where wedges are employed, by coating the surface of the slots in which the wedges proximate the q axis are placed with a material having a higher electrical conductivity than that of the wedges, (v) where damper bars are employed, providing that the width of the openings of the slots proximate the d axis is less than the width of the openings of the slots proximate the q axis. Thus, the beneficial effects of the invention can be obtained through the provision of dissimilar wedges or damper bars. According to preferred embodiments of the present invention as defined above, the resistance loss distribution over the entire rotor surface in the circumferential direction can be uniformalized and thermal balance over the entire rotor surface can be achieved. As a result, resistance to higher harmonics of the turbine generator is significantly improved, and accordingly a correspondingly larger current can be passed safely through the armature windings of the turbine generator. Hence the time needed to start the turbine can be reduced. The present invention relates to a turbine generator, and to the generator per se. Embodiments of the present invention will now be described, by way of example, by reference to the accompanying drawings, in which: Fig.1 is a cross sectional view of a turbine generator rotor illustrating one embodiment according to the present invention ; Fig.2 is a diagram illustrating a combined cycle electric power generation system relating to the present invention ; Fig.3 is a diagram illustrating a turbine generator system with a thyristor type starting device relating to the present invention ; Fig.4(a) and Fig.4(b) are diagrams illustrating armature currents fed from the thyristor type starting device relating to the present invention, wherein Fig.4(a) is a diagram illustrating armature current waveforms of 120° electrical angle conduction period and Fig.4(b) is a diagram illustrating a spectrum characteristic of the armature current ; Fig.5 is a diagram illustrating a relationship between magnetomotive force vectors in the machine of the turbine generator during starting with thyristors relating to the present invention ; Fig.6 is a diagram for explaining a magnetomotive force induced by higher harmonics during starting with thyristors relating to the present invention ; Fig.7 is a partially broken perspective view illustrating a schematic structure of a turbine generator relating to the present invention ; Fig.8 is a cross sectional view of a turbine generator rotor illustrating another embodiment according to the present invention ; Fig.9 is a cross sectional view of a turbine generator rotor illustrating still another embodiment according to the present invention ; Fig.10 is a cross sectional view of a turbine generator rotor illustrating a further embodiment according to the present invention ; Fig.11 is a cross sectional view of a turbine generator rotor illustrating a still further embodiment according to the present invention ; Fig.12 is a cross sectional view of a turbine generator rotor illustrating a still further embodiment according to the present invention ; Fig.13 is a cross sectional view of a turbine generator rotor illustrating a still further embodiment according to the present invention ; Fig.14 is a cross sectional view of a turbine generator rotor illustrating a still further embodiment according to the present invention ; and Fig.15 is a cross sectional view of a turbine generator rotor illustrating a still further embodiment according to the present invention. Hereinbelow, the embodiments of the present invention are explained in detail with reference to the drawings. Fig.1 shows a rotor of a turbine generator illustrating one embodiment of the present invention. Fig.7 shows a structure of a turbine generator relating to the present invention. In the drawings, numeral 2 denotes a rotor, numeral 3 rotor slots for accommodating field windings, numeral 4 wedges at the side of magnetic poles (d axis) of the rotor 2, and numeral 5 wedges at the side between the magnetic poles (q axis) of the rotor 2. In the present embodiment, the generator is a rotating field type turbine generator in which a stator 16 is formed by a laminated iron core and is provided with armature windings 18. The rotor 2 is a solid iron core of cylindrical shape, the field windings are provided in the slots 3 and are held in the slots 3 via the wedges 4, 5. The manner of uniformalizing the resistance loss distribution over the surface of the rotor 2 by varying the configuration of the wedges during starting with thyristors is explained with reference to Fig.1. The wedges 4 and 5 are formed with metal bars with no joints in order to enhance their damper effect and their both ends are connected to respective short circuiting rings. During starting with thyristors since an elliptic rotating magnetic field having the longer diameter on d axis and the shorter diameter on q axis is generated, a larger eddy current is induced at the side between the magnetic poles on the rotor 2 than at the side on the magnetic poles on the rotor 2. Therefore, the thickness d' in radial direction of the wedges 5 positioned at the side between the magnetic poles on the rotor 2 is determined larger than the thickness d in radial direction of the wedges 4 at the side of the magnetic poles on the rotor 2 so as to reduce the resistance of the wedges 5 at the side on q axis. Since the magnitude of eddy current flowing through the respective wedges is substantially determined by their positions of the respective wedges, by means of reducing the resistance of the wedges 5 positioned at the side between the magnetic poles where a large eddy current tends to flow, the resistance loss distribution over the surface of the rotor 2 in circumferential direction is uniformalized. Accordingly, a thermal balance over the entire surface on the rotor 2 is achieved, as a result, the resistance to higher harmonics of the generator during starting thereof is improved and a correspondingly large current can be fed to the armature windings, thereby the starting time thereof can be reduced. Fig.8 shows a rotor of a turbine generator illustrating another embodiment according to the present invention. A manner of uniformalizing the resistance loss distribution over the surface of the rotor 2 in circumferential direction during starting with thyristors by varying the configuration of the damper bars is explained with reference to the present embodiment. In the drawing, numeral 2 denotes a rotor, numeral 3 rotor slots, numeral 6 wedges having short axial length, numeral 7 damper bars positioned at the side of the magnetic poles and numeral 8 damper bars positioned at the side between the magnetic poles. The rotor 2 of a rotating magnetic field type turbine generator is provided with the slots 3 for accommodating field windings, the wedges 6 of short axial length for holding the field windings, the damper bars 7 positioned at the side of the magnetic poles on the rotor 2 and the damper bars 8 positioned at the side between the magnetic poles on the rotor 2. Further, in the present embodiment the thickness d' in radial direction of the damper bars 8 positioned at the side between the magnetic poles on the rotor 2 is determined larger than the thickness d in radial direction of the damper bars 7 at the side of the magnetic poles on the rotor 2 so as to reduce the resistance of the damper bars 8. As a result, substantially the same advantage as obtained in connection with the Fig.1 embodiment is obtained with the present embodiment. Fig.9 shows a rotor of a turbine generator illustrating still another embodiment according to the present invention. A manner of uniformalizing the resistance loss distribution over the surface of the rotor 2 in circumferential direction during starting with thyristors by varying the physical properties of the wedges is explained with reference to the present embodiment. In the present embodiment the rotor 2 of a rotating field type turbine generator is provided with the slots 3 for accommodating the field windings and wedges 4 and 5 in a form of metal bars with no joints and having a damper winding effect, and the both ends of the respective wedges 4 and 5 are connected via corresponding short circuiting rings. Herein, the wedges 4 are ones positioned at the side of the magnetic poles on the rotor 2 and the wedges 5 are ones positioned at the side between the magnetic poles on the rotor 2. Further, in the present embodiment, when assuming that the resistivity of the wedges 4 positioned at the side of the magnetic poles on the rotor 2 as ρ and the resistivity of the wedges 5 positioned at the side between the magnetic poles as ρ ', wedge materials having a relationship of ρ > ρ ' are used so as to reduce the resistance of the wedges 5 positioned at the side between the magnetic poles on the rotor 2. Examples of material combinations which satisfy the above relationship of ρ > ρ ' are aluminium or aluminum alloy for the wedges 4 and copper or copper alloy for the wedges 5, iron for the wedges 4 and aluminium or aluminium alloy for the wedges 5, iron for the wedges 4 and copper for the wedges 5, and iron for the wedges 4 and copper alloy for the wedges 5. As a result, substantially the same advantages as obtained in connection with the Fig.1 embodiment is obtained with the present embodiment. Fig.10 shows a rotor of a turbine generator illustrating a further embodiment according to the present invention. A manner of uniformalizing the resistance loss distribution over the surface of the rotor 2 in circumferential direction during starting with thyristors by varying the physical properties of the damper bars is explained with reference to the present embodiment. In the present embodiment, the rotor 2 of a rotating field type turbine generator is provided with the slots 3 for accommodating the field windings and wedges 6 of short axial length for retaining the field windings, damper bars 7 positioned at the side of the magnetic poles on the rotor 2 and the damper bars 8 positioned at the side between the magnetic poles on the rotor 2. Further, in the present embodiment, when assuming that the resistivity of the damper bars 7 positioned at the side of the magnetic poles on the rotor 2 as ρ and the resistivity of the damper bars 8 positioned at the side between the magnetic poles as ρ ', damper bar materials having a relationship of ρ > ρ ' are used so as to reduce the resistance of the damper bars 8 positioned at the side between the magnetic poles on the rotor 2. Examples of material combinations which satisfy the above relationship of ρ > ρ ' are the same as in the examples in Fig.9 embodiment and substantially the same advantages as obtained in connection with the Fig.1 embodiment is likely obtained with the present embodiment. Fig.11 shows a rotor of a turbine generator illustrating a still further embodiment according to the present invention. A manner of uniformalizing the resistance loss distribution over the surface of the rotor 2 in circumferential direction during starting with thyristors by varying the configuration of the wedges is explained with reference to the present embodiment. In the present embodiment the rotor 2 of a rotating field type turbine generator is provided with the slots 3 for accommodating the field windings and wedges 4 and 5 in a form of metal bars with no joints and having a damper winding effect, and the both ends of the respective wedges 4 and 5 are connected via corresponding short circuiting rings. Herein, the wedges 4 are ones positioned at the side of the magnetic poles on the rotor 2 and the wedges 5 are ones positioned at the side between the magnetic poles on the rotor 2. Further, in the present embodiment, the width x' in circumferential tirection of the wedges 5 positioned between the magnetic poles of the rotor 2 is determined larger than the width x in circumferential direction of the wedges 4 positioned at the portions of the magnetic poles without varying the spacing distance between adjacent slot bottoms positioned between the magnetic poles on the rotor 2 to thereby reduce the resistance of the wedges 5. In the present embodiment, the slot opening width s' positioned between the magnetic poles on the rotor 2 can be determined either larger than or equal to the slot opening width s positioned at the portions of the magnetic poles on the rotor 2. As a result, substantially the same advantages as obtained in connection with the Fig.1 embodiment is obtained with the present embodiment. Fig.12 shows a rotor of a turbine generator illustrating a still further embodiment according to the present invention. A manner of uniformalizing the resistance loss distribution over the surface of the rotor 2 in circumferential direction during starting with thyristors by varying the configuration of the damper bars is explained with reference to the present embodiment. In the present embodiment, the rotor 2 of a rotating field type turbine generator is provided with the slots 3 for accommodating the field windings and wedges 6 of short axial length for retaining the field windings, damper bars 7 positioned at the side of the magnetic poles on the rotor 2 and the damper bars 8 positioned at the side between the magnetic poles on the rotor 2. Further, in the present embodiment, the opening width s' of the slots 3 positioned between the magnetic poles on the rotor 2 is determined larger than the opening width s of the slots 3 positioned at the portions of the magnetic poles on the rotor 2 as well as the width in circumferential direction of the damper bars 8 positioned between the magnetic poles on the rotor 2 is determined larger than the width in circumferential direction of the dsamper bars 7 positioned at the portions of the magnetic poles on the rotor 2 without varying the spacing distance between adjacent slot bottoms positioned between the magnetic poles on the rotor 2, thereby the resistance of the damper bars 8 positioned between the magnetic poles on the rotor 2 is reduced and substantially the same advantages as obtained in connection with the Fig.1 embodiment is likely obtained with the present embodiment. Fig.13 shows a rotor of a turbine generator illustrating a still further embodiment according to the present invention. A manner of uniformalizing the resistance loss distribution over the surface of the rotor 2 in circumferential direction during starting with thyristors by varying the configuration of the wedges is explained with reference to the present embodiment. In the present embodiment the rotor 2 of a rotating field type turbine generator is provided with the slots 3 for accommodating the field windings and wedges 4 and 5 in a form of metal bars with no joints and having a damper winding effect, and the both ends of the respective wedges 4 and 5 are connected via corresponding short circuiting rings. Herein, the wedges 4 are ones positioned at the side of the magnetic poles on the rotor 2 and the wedges 5 are ones positioned at the side between the magnetic poles on the rotor 2. Further, in the present embodiment, the surface facing the gap of the wedges 5 positioned between the magnetic poles on the rotor 2 is coated with a material having a higher electrical conductivity than that of the wedges 4 and 5. Namely, when the wedges 4 and 5 are made of iron, copper, copper alloy or aluminium is selected for the coating material and when the wedges 4 and 5 are made of aluminium, copper or copper alloy is selected for the coating material. With thus constituting, substantially the same advantages as obtained in connection with Fig.1 embodiment is likely obtained with the present embodiment. Fig.14 shows a rotor of a turbine generator illustrating a still further embodiment according to the present invention. A manner of uniformalizing the resistance loss distribution over the surface of the rotor 2 in circumferential direction during starting with thyristors by differentiating damper effects on d axis and q axis is explained with reference to the present embodiment. In the present embodiment, the rotor 2 of a rotating field type turbine generator is provided with slots 3 for accommodating the field windings and wedges 4 and 5 in a form of metal bars with no joints and having a damper effect. Further, in the present embodiment, the rotor 2 is further provided with additional wedges 5 along the teeth portions positioned between the magnetic poles on the rotor 2. The wedges 5 positioned on q axis have a large damper effect against magnetic fluxes of higher harmonics directing in d axis but have no damper effect against magnetic fluxes of higher harmonics directing in q axis. Accordingly, an damper effect against the magnetic fluxes of higher harmonics directing in d axis on the rotor 2 is strengthened and the burden of the respective wedges 5 sharing the eddy current flowing therethrough is reduced, the resistance loss distribution over the entire surface of the rotor 2 is uniformalized and a thermal balance over the entire surface on the rotor 2 is achieved. As a result, the resistance to higher harmonics of the generator during starting thereof is improved, and a correspondingly large current can be fed to the armature windings, thereby the starting time thereof can be reduced. Fig.15 shows a rotor of a turbine generator illustrating a still further embodiment according to the present invention. A manner of uniformalizing the resistance loss distribution over the surface of the rotor 2 in circumferential direction during starting with thyristors by differentiating damper effects on d axis and q axis is explained with reference to the present embodiment. In the present embodiment, the rotor 2 of a rotating field type turbine generator is provided with slots 3 for accommodating the field windings, wedges 6 of short axial length for retaining the field windings, damper bars 7 positioned at the side of the magnetic poles on the rotor 2 and the damper bars 8 positioned at the side between the magnetic poles on the rotor 2. Further, in the present embodiment, the rotor 2 is further provided with additional damper bars 8 along the teeth portions positioned between the magnetic poles on the rotor 2. Accordingly, the burden of the respective damper bars 8 sharing the eddy current flowing therethrough is reduced, and substantially the same advantages obtained in Fig.14 embodiment are likely obtained with the present embodiment. In the above embodiments, rotors having two poles and eight slots are illustrated. However, the present invention can be likely applied to rotors having any number of poles and any number of slots. According to the present invention as explained herein above, the elliptic rotating magnetic field which is caused in the machine during starting by making use of thyristors is suppressed by the damper windings, thereby a thermal balance over the entire portions on the rotor of the turbine generator can be achieved and the resistance against higher harmonics thereof is improved. As a result, a correspondingly large current can be fed to the armature windings and thereby the starting time thereof can be reduced.

Claims: A turbine generator comprising a stator (16) having armature windings (18), and a rotor (2) disposed facing said stator (16) and provided with a plurality of axially extending slots (3) arranged circumferentially with a predetermined interval, field windings disposed in said slots (3) and wedges (4,5) having a damper effect inserted in said slots (3) so as to retain said field windings therein, and optionally damper bars within the slots, characterized in that, taking the direction of magnetomotive force of said field windings as the d axis and the direction perpendicular to the d axis as the q axis, the physical properties or the configuration of said wedges (5) or, where provided, damper bars (8) positioned proximate the q axis on said rotor (2) are varied from the physical properties or the configuration of said wedges (4) or damper bars (7) positioned proximate the d axis on said rotor (2) in such a manner that the resistance of the wedges (5) or damper bars (8) positioned proximate the q axis is smaller than the resistance of the wedges (4) or damper bars (7) proximate the d axis and the heating of the respective wedges (4,5) or damper bars (7,8) due to resistance loss caused by current flowing therethrough during starting with thyristors of the turbine generator is uniformalized in the circumferential direction of said rotor (2), and a thermal balance between said wedges (5) or damper bars (8) positioned proximate the q axis on said rotor (2) and said wedges (4) or damper bars (7) positioned proximate the d axis on said rotor (2) is maintained during starting with thyristors of the turbine generator. A turbine generator according to claim 1, wherein, the radial thickness of wedges (4) or, where provided, damper bars (7), proximate the d axis is less than the radial thickness of wedges (5) or damper bars (8) proximate the q axis. A turbine generator according to claim 1, wherein, the resistivity of wedges (4) or, where provided, damper bars (7), proximate the d axis is greater than the resistivity of wedges (5) or damper bars (8) proximate the q axis. A turbine generator according to claim 1, wherein, the width in the circumferential direction of wedges (4) proximate the d axis is less than the width in the circumferential direction of wedges (5) proximate the q axis. A turbine generator according to claim 1, wherein, the stator-facing surface of wedges (5) proximate the q axis being coated with a material having a higher electrical conductivity than that of said wedges (4,5). A turbine generator according to claim 1, wherein, damper bars being provided, the width in the circumferential direction of damper bars (7) proximate the d axis is less than the width in the circumferential direction of damper bars (8) proximate the q axis and further opening width of slots (3) proximate the d axis is less than the opening width of slots (3) proximate the q axis. A turbine generator according to claim 1, wherein, the resistance of wedges (5) positioned proximate the q axis is smaller than the resistance of wedges (4) proximate the d axis, further wedges (5) having a damper effect being provided along teeth portions proximate the q axis. A turbine generator according to claim 1, having damper bars, said damper bars (7,8) being constituted so as to differentiate their damper effect at d axis and q axis on said rotor (2). A turbine generator according to claim 1, wherein, damper bars being provided, the resistance of damper bars (8) positioned proximate the q axis is smaller than the resistance of damper bars (7) proximate the d axis, further damper bars (8) being provided along teeth portions proximate the q axis.

Inventors: IDE KAZUMASA, KOHARAGI HARUO, MIYAKAWA KADO, TAKAHASHI MIYOSHI, WAKUI SHINICHI, YAGI YASUOMI, IDE, KAZUMASA, KOHARAGI, HARUO, MIYAKAWA, KADO, TAKAHASHI, MIYOSHI, WAKUI, SHINICHI, YAGI, YASUOMI
Applicants: HITACHI LTD, HITACHI, LTD.
Application year: 1994
Main classification: H02K1
IPC codes: H02K3, H02K19, H02K1